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Ching-Pang Lee
Ching-Pang
Lee
F - Mech Eng,Light,Heat,Weapons
02
K
Inventor
Country: United States Of America
Affiliated with
A turbine assembly for a gas turbine engine and method of...
F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
[ 0.00 ] – not rated yet
Aft entry cooling system and method for an aircraft engine
F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
[ 0.00 ] – not rated yet
Airfoil leading edge end wall vortex reducing plasma
F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
[ 0.00 ] – not rated yet
Angled turbulence promoter
F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
[ 0.00 ] – not rated yet
Article surface with metal wires and method for making
F - Mech Eng,Light,Heat,Weapons – 28 – F
Patent
[ 0.00 ] – not rated yet
Also associated with
Aft entry cooling system and method for an aircraft engine
F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
[ 0.00 ] – not rated yet
Compound nozzle cooled engine
F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
[ 0.00 ] – not rated yet
Film cooling of jet engine components
F - Mech Eng,Light,Heat,Weapons – 02 – K
Patent
[ 0.00 ] – not rated yet
Internally cooled airfoil blade
F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
[ 0.00 ] – not rated yet
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Profile ID: LFCA-PAI-P-1130196
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